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https://apps.dtic.mil/sti/pdfs/ADA414407.pdf
150°C for 65 hours. Discussion Microstructural Evolution Mechanisms As-cast grain boundaries are pancaked, and subgrains are formed during the rolling of cast Al-Li ingot into a plate product form. For Al alloys containing coherent AlgZr dispersoids, it is difficult to break
https://www.tinker.af.mil/News/Article-Display/Article/2838589/air-force-research-laboratory-partners-with-google-cloud-to-accelerate-collabor/
WASHINGTON, D.C. AND DAYTON, OHIO – Google Cloud announced November 3 that the Air Force Research Laboratory has chosen to deploy Google Workspace as a pilot program among a segment of its workforce of scientists and engineers. The initial deployment has dramatically enhanced engagement with its worldwide network of external research partners.
https://apps.dtic.mil/dtic/tr/fulltext/u2/a458861.pdf
Metals Branch (AFRL/MLLM) Metals, Ceramics, and Nondestructive Evaluation Division Materials and Manufacturing Directorate Air Force Research Laboratory, Air Force Materiel Command Wright-Patterson Air Force Base, OH 45433-7750 9. SPONSORING/MONITORING AGENCY NAME(S) AND ADDRESS(ES) 10. SPONSORING/MONITORING AGENCY ACRONYM(S) AFRL-ML …
https://apps.dtic.mil/dtic/tr/fulltext/u2/a463095.pdf
³Air Force Research Laboratory, AFRL/MLLM, Wright-Patterson AFB, OH 45433 4 Universal Technology Corporation, Dayton, OH 45432 Abstract - A new Taylor-type polycrystalline model has been developed to simulate the evolution of crystallographic texture and the anisotropic stress-strain response during large
https://centers.hpc.mil/systems/status.html
After Hours: Calls, e-mails and tickets received after normal operating hours will be addressed the following business day. Mailing Address: DoD HPCMP HPC Help Desk AFRL/RCM 2435 Fifth Street Wright-Patterson Air Force Base, OH - 45433-7802 Ticket Requests
https://www.tms.org/superalloys/10.7449/2005/Superalloys_2005_35_45.pdf
982°C for 4 hours followed by polymer quenching and a 788°C/8hr/furnace cool primary age and a 704°C/8hr/air cool secondary age sequence. Microstructures were evaluated in 10 locations on two diametrically opposed cross sections. Grain sizes were evaluated according to
https://www.tms.org/Superalloys/10.7449/2004/Superalloys_2004_887_896.pdf
Air Force Research Laboratory, AFRL/MLLM Materials and Manufacturing Directorate Wright-Patterson AFB OH 45433-7817 Keywords: Yield Strength, Superalloys, Model, Spreadsheet Alloys: Nimonic105, IN100, René88, Alloy ME3 Abstract Simulation methods allow the possibility of overcoming some of the deficiencies of analytical models.
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